US4390082A - Reserve lubricant supply system - Google Patents
Reserve lubricant supply system Download PDFInfo
- Publication number
- US4390082A US4390082A US06/217,572 US21757280A US4390082A US 4390082 A US4390082 A US 4390082A US 21757280 A US21757280 A US 21757280A US 4390082 A US4390082 A US 4390082A
- Authority
- US
- United States
- Prior art keywords
- pressure
- pressurized
- supply system
- gas
- lubricant supply
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000314 lubricant Substances 0.000 title claims abstract description 89
- 238000004891 communication Methods 0.000 claims description 8
- 230000001105 regulatory effect Effects 0.000 abstract description 4
- 230000004308 accommodation Effects 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 40
- 239000007788 liquid Substances 0.000 description 3
- 238000005461 lubrication Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000001050 lubricating effect Effects 0.000 description 2
- 230000000740 bleeding effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000012858 resilient material Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/18—Lubricating arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M1/00—Pressure lubrication
- F01M1/16—Controlling lubricant pressure or quantity
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/12—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
- F16C17/24—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with devices affected by abnormal or undesired positions, e.g. for preventing overheating, for safety
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/06—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
- F16C32/0629—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a liquid cushion, e.g. oil cushion
- F16C32/064—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a liquid cushion, e.g. oil cushion the liquid being supplied under pressure
- F16C32/0644—Details of devices to control the supply of liquids to the bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/06—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
- F16C32/0681—Construction or mounting aspects of hydrostatic bearings, for exclusively rotary movement, related to the direction of load
Definitions
- the present invention relates to lubrication systems for machinery.
- Pressurized lubricating systems have long been used with machinery employing bearings and the like to reduce the friction and wear between machinery parts sliding on one another. Many of these systems are incapable of operating for even a relatively short period of time without the lubricant in a pressurized state.
- reserve lubricant supply systems have been employed which provide the required pressurized lubricant during shutdown of the equipment. Often, a reserve reservoir of oil is pressurized on a standby basis by a reserve pump, an elevated location for the lubricant reservoir or a pressurized body of compressed gas.
- a compressed body of gas is a most popular form of pressurizing mechanism and employs a vessel to act as the reserve oil reservoir, a bladder within the vessel, and pressurized nitrogen or the like in the bladder.
- the vessel is in communication with the main oil supply and, thus, is held under the same pressure as the main oil supply during nominal operation.
- the amount of gas contained within the bladder is such that a pressure equilibrium between the inside of the bladder and the surrounding vessel is reached with the bladder substantially deflated. When the main oil supply pressure fails, the bladder then expands as the pressure drops, and forces the reserve oil from the reserve vessel.
- the expansion of the gas within the bladder from 1,000 p.s.i. to 950 p.s.i. displaces an amount of oil which is equal to only 5% of the volume of the gas prior to expansion. If the vessel is divided equally between oil reservoir volume and bladder volume, only 2.5% of the vessel's volume of oil is available in the usable range. If the vessel has a total capacity of ten gallons, the usable supply of oil at or above 950 p.s.i. is only one quart of oil. In the type of equipment in which such systems are employed, a normal rate of oil usage may be twenty gallons per minute. The bearing would thus be supplied with emergency oil for less than one second. A more normal shutdown time for such equipment is on the order of five to thirty seconds. Thus, reserve systems as described above are inadequate.
- the present invention is directed to a system for providing pressurized reserve lubricant where a substantial drop in the pressure of the reserve lubricant during its use cannot be tolerated.
- the system is employed in machinery where external pressure is applied to at least one side of a bearing such as in large pumps, turbines, turbo-expanders, or the like.
- the external pressure is employed by the reserve system in supplying relatively uniform pressure to the reserve oil supply.
- the pressure thus supplied to the reserve system may be regulated where necessary by critical pressure conditions within the main system, e.g., the pressure of the main lubricant supply or the pressure at the lubricant exhaust from the bearing or bearings. If pressures are relatively predictable in the main system, the regulation may be by a preset, fixed setting rather than as a function of one of the condition within the system.
- the present system is most useful with a rotary device, such as a centrifugal pump, which employs a pressurized gas seal to protect the bearings. Pressure from the seal may then be used as a source of pressure for the reserve lubricant system.
- FIG. 1 is a schematic view of a device which may be employed with the present invention.
- FIG. 2 is a schematic detail of one arrangement of the present invention.
- FIG. 3 is a schematic detail of another arrangement of the present invention.
- Each bearing 14 and 16 includes an annular cavity 20 and 22, into which pressurized lubricant may be forced.
- the pressurized lubricant will then flow, in the case of bearing 14, into chambers 24 and 26.
- the pressurized oil will flow along the main shaft 10 to chambers 26 and 28.
- Chambers 26 and 28 are connected by a passageway 30, and are allowed to drain via a conduit 32 into a main reservoir 34.
- the chamber 24 drains into a preservoir chamber 36.
- Labyrinth seals are provided outwardly of each of the bearings 14 and 16.
- the labyrinth seal 38 outwardly of bearing 16 and chamber 28 is of simple construction.
- Labyrinth seal 40 outwardly of bearing 14 and chamber 24 includes a pressurized gas seal.
- the pressurized gas seal includes an annular cavity 42 which may be pressurized through line 44. Buffer gas is introduced through line 44 into the annular cavity 42 which is at a higher pressure than the prevailing pressure in the chamber 24 and in the rotor cavity 46 adjacent to the seal 38. In this way, a buffer gas may be selected which is compatible with both the lubricant flowing into the chamber 24 and the material being processed by the rotor 12.
- the rotor cavity 46 determines the pressure at which the buffer gas must be maintained. If no pressure were maintained within the chamber 24, flow of the buffer gas into chamber 24 would be controlled only by the labyrinth seal 40. However, a restriction is placed on the outlet from the chamber 36 which has an effect of controlling this flow. As the chamber 24 only vents through the chamber 36, an orifice 48 may be used on a gas vent 50 to provide sufficient restriction to reduce the flow of gas from the annular cavity 42 into the chamber 36 through the labyrinth seal 40. A liquid outlet 52 must also be controlled for the chamber 36 to maintain the proper restriction to gas flow through the orifice 48.
- the liquid outlet 52 includes a valve 54 controlled by a float 56. As the chamber 36 fills with lubricant from the bearing 14, the float 56 rises and actuates the valve 54 such that an appropriate amount of lubricant is discharged through the liquid outlet 52 to the reservoir 34.
- the pressurized main lubricant supply for the bearings 14 and 16 includes a pump 58 which may be conveniently driven by a motor 60 and draws lubricant from the main reservoir 34.
- the pressurized pump discharge is conveyed through line 62 to line 64 and 66 which in turn supply the annular cavities 20 and 22 of the bearings 14 and 16.
- lubricant is forced by the pump 58 to flow in a continuous path to the clearances between the bearings 14 and 16 and the shaft 10, then into the several chambers 24, 26 and 28, to the reservoir 34 and then again to the pump 58.
- the pressure provided by the pump 58 must, of course, be sufficient to provide the requisite lubricating film in the bearings 14 and 16 and must also be higher than the pressure existing in the chamber 24. The latter condition is normally met by adjusting the pressure on the pump 58 rather than by varying the size of the orifice 48 associated with the gas vent 50.
- a reserve lubricant supply is provided.
- the reserve lubricant supply is provided by a reserve lubricant reservoir 68 which is in open communication with the pressurized supply line 62 of the main lubricant system by means of a passageway 70.
- a check valve 72 is provided in the pressurized supply line of the main lubricant system to insure that the pressure and flow from the reserve lubricant reservoir 68 when activated will be toward the bearings 14 and 16.
- the volume of the reservoir 68 is sized to provide sufficient lubricant during the expected period of shutdown of the mechanism with which it is associated.
- the gas pressurized chamber Located within the reserve lubricant reservoir 68 is a gas pressurized chamber which has an expansible wall common with the reservoir 68 so that the volume of the reservoir can be controlled by the gas pressure within the gas pressurized chamber.
- the gas pressurized chamber includes a bladder 74 of sufficiently resilient material such that it can be collapsed to substantially no volume or expanded to force lubricant from the reservoir 68.
- the change in volume of which the bladder 74 is capable should at least equal the volume of the lubricant required to maintain adequate lubrication of the bearings 14 and 16 during the expected shutdown.
- the bladder 74 is associated with a gas pressure source line 76.
- a pressure meter 78 provides easy monitoring of the pressure to the bladder 74.
- the gas pressure source line 76 receives pressure from a continuous source of pressure associated with the mechanism.
- This continuous source of pressure may either be the pressurized gas seal or the rotor cavity of the lubricated machinery. If pressure is received from the pressurized gas seal, the pressure may be received from either the supply to the seal or at an intermediate point along the labyrinth seal 40 at a distance from the annular cavity 42. In the first case, pressure would be taken from line 80 associated with line 44 and in the second case pressure would be taken from line 82. Alternately, pressure existing in the rotor cavity may be employed via line 84.
- one of lines 80, 82 and 84 would be coupled with gas pressure source line 76 to supply gas to the bladder 74.
- the resulting pressure to the bladder 74 must be less than the pressure existing in the pressurized supply line 62 of the main lubricant supply system during normal operation thereof. This insures that the bladder 74 will be collapsed and the reserve lubricant reservoir 68 fully charged. This may be accomplished by insuring that the pressure takeoff from the pressurized gas seal or from the rotor cavity is at a location where the pressure derived therefrom will be lower than that in the line 62. Alternately, a regulator may be employed in the gas pressure source line 76.
- the takeoff may be via line 80. If such is not the case, the takeoff may be via line 82 which insures a pressure drop from that of the supply pressure to the gas seal.
- Such an intermediate takeoff in the gas seal into insures that the pressure so derived will be above that of the chamber 24. It is of benefit to have the operative pressure for the bladder 74 be above that of the chamber 24 in order that lubricant will flow from the annular cavity 20 in the bearing 14 toward the chamber 24.
- the gas pressure source is derived from the rotor cavity, the source may be moved radially inwardly or outwardly in that cavity to optimize the desired pressure.
- a regulator 86 may be employed.
- the regulator may be set at a fixed pressure or may be controlled through a line 87 by either the pressure existing in the supply line 62 of the main lubricant system through at tap 89 or the pressure existing in the chamber 24 through a tap 91.
- the regulator must be set to maintain pressure in the bladder 74 at a pressure below that of the regulating pressure. In the case of the chamber 24, the regulator must be set so that the pressure in the bladder 74 is higher than the regulating pressure. In either event, the pressure in the bladder 74 during normal operation of the main lubricant supply system is to be maintained at a pressure between the supply pressure of the main lubricant supply system and the discharge pressure existing in chamber 24.
- an additional element, orifice 88 is included in the system. This orifice accomodates temporary overpressure situations which may possibly occur. Without the orifice 88, an overpressure condition would simply be maintained by the regulator 86. With the orifice 88 slowly bleeding off pressure, the regulator 86 will be required to again periodically operate to supply more pressure to the reserve system. If the overpressure is a temporary condition, the regulator 86 will readjust to the appropriate pressure level. To provide a slow bleed off of pressure, the orifice 88 preferably provides a restriction to flow which is substantially greater than the total effective restriction between the bladder 74 and the source of pressurized air. Thus, the orifice cannot significantly reduce the flow to the bladder 74 when needed.
- FIG. 3 also illustrates additional equipment associated with the reserve lubricant supply system.
- Associated with the regulator 86 is a gas reservoir 92.
- the combination of the orifice 90 and the reservoir 92 help to overcome any leaks which may exist in the system by delaying the loss of pressure and buffer and delay any change in pressure in gas supply to the bladder 74.
- a main lubricant supply system is employed to distribute lubricant to a mechanism. As it is operating normally, it will supply lubricant to the reserve lubricant supply system and collapse the bladder 74 which is maintained at a pressure below that of the supply line of the main lubricant supply system.
- the maintenance of the pressure in the bladder 74 is undertaken either by insuring the pressure delivered to the bladder never exceeds that of the lubricant supply by employing sources of pressure such as the gas seal and the rotor cavity at points where the pressure does not rise above that of the lubricant supply or by regulation of the pressure as measured by the main lubricant supply pressure or the pressure of the lubricant discharge from the bearing.
- the mechanism When the main system fails, the mechanism is shut down, and during the shutdown period the check valve 72 automatically closes and the pressure supplied to the bladder 74 forces pressure into the main lubricant supply line from the reserve system and into the bearings. As the source of pressure is not immediately exhausted, the full expansion of the bladder 74 will occur at pressures which are required to adequately supply the bearings. In this way, a failure of the main lubricant supply system can occur without damage to the mechanism being lubricated.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims (14)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/217,572 US4390082A (en) | 1980-12-18 | 1980-12-18 | Reserve lubricant supply system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/217,572 US4390082A (en) | 1980-12-18 | 1980-12-18 | Reserve lubricant supply system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US4390082A true US4390082A (en) | 1983-06-28 |
Family
ID=22811623
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US06/217,572 Expired - Lifetime US4390082A (en) | 1980-12-18 | 1980-12-18 | Reserve lubricant supply system |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US4390082A (en) |
Cited By (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4511016A (en) * | 1982-11-16 | 1985-04-16 | Mtu Motoren-Und Turbinen-Union Muenchen Gmbh | Lubricating system for gas turbine engines |
| US4697414A (en) * | 1985-12-09 | 1987-10-06 | The Garrett Corporation | Lubrication apparatus |
| US4739862A (en) * | 1986-03-21 | 1988-04-26 | Mullis H Leon | Pressure lubricator |
| US4741155A (en) * | 1985-12-09 | 1988-05-03 | Allied-Signal Inc. | Lubrication method and apparatus |
| WO1988009874A1 (en) * | 1987-06-12 | 1988-12-15 | Kletschka Harold D | Rotary pump with a coupling section |
| US4856273A (en) * | 1988-07-21 | 1989-08-15 | General Motors Corporation | Secondary oil system for gas turbine engine |
| US4858426A (en) * | 1988-07-21 | 1989-08-22 | General Motors Corporation | Secondary oil system for gas turbine engine |
| US4858427A (en) * | 1988-08-08 | 1989-08-22 | General Motors Corporation | Secondary oil system for gas turbine engine |
| US4888947A (en) * | 1988-10-31 | 1989-12-26 | General Motors Corporation | Secondary oil system |
| US4891934A (en) * | 1988-10-31 | 1990-01-09 | General Motors Corporation | Oil system for gas turbine engine |
| US5040366A (en) * | 1989-01-13 | 1991-08-20 | General Electric Company | Fluid transfer device |
| US5147015A (en) * | 1991-01-28 | 1992-09-15 | Westinghouse Electric Corp. | Seal oil temperature control method and apparatus |
| WO1999020880A1 (en) * | 1997-10-23 | 1999-04-29 | Carl Fredriksson | Device, method and application in connection with a turbomachine and pumping and lubricating arrangement in connection with such a machine |
| US20050000753A1 (en) * | 2003-07-03 | 2005-01-06 | Sheridan William G. | Failure tolerant passive lubrication system |
| US20050034924A1 (en) * | 2003-08-14 | 2005-02-17 | James Denman H. | Emergency lubrication system |
| US20050139427A1 (en) * | 2002-03-01 | 2005-06-30 | Alain Antonetti | Gear mechanism with controlledl device for generating a rarefied atmosphere |
| US7216473B1 (en) * | 1999-07-09 | 2007-05-15 | Hamilton Sundstrand Corporation | Turbojet engine lubrication system |
| US20090057060A1 (en) * | 2007-08-28 | 2009-03-05 | Hamilton Sundstrand Corporation | Recirculating lubrication system with sealed lubrication oil storage |
| US20090324151A1 (en) * | 2008-06-30 | 2009-12-31 | Nucor Corporation | Slew bearing system |
| US20110163018A1 (en) * | 2010-01-04 | 2011-07-07 | General Electric Company | Hydrogen cooled generator lubricant drain system |
| US20130086903A1 (en) * | 2011-10-06 | 2013-04-11 | Gm Global Technology Operations Llc. | Engine assembly including fluid control to boost mechanism |
| US9127567B2 (en) | 2012-06-29 | 2015-09-08 | United Technologies Corporation | Non-interrupted turbomachine fluid supply |
| US9151327B2 (en) | 2010-06-11 | 2015-10-06 | Siemens Aktiengesellschaft | Backup lubrication system for a rotor bearing |
| EP3036470A4 (en) * | 2013-08-20 | 2016-08-17 | United Technologies Corp | Emergency oil system |
| US20170314419A1 (en) * | 2014-11-03 | 2017-11-02 | Echogen Power Systems, L.L.C. | Active thrust management of a turbopump within a supercritical working fluid circuit in a heat engine system |
| US10934895B2 (en) | 2013-03-04 | 2021-03-02 | Echogen Power Systems, Llc | Heat engine systems with high net power supercritical carbon dioxide circuits |
| US11187112B2 (en) | 2018-06-27 | 2021-11-30 | Echogen Power Systems Llc | Systems and methods for generating electricity via a pumped thermal energy storage system |
| US11293313B2 (en) * | 2018-09-19 | 2022-04-05 | Saudi Arabian Oil Company | Turbomachinery lubrication system improvement gravity rundown tanks |
| US11435120B2 (en) | 2020-05-05 | 2022-09-06 | Echogen Power Systems (Delaware), Inc. | Split expansion heat pump cycle |
| US20230030818A1 (en) * | 2021-07-30 | 2023-02-02 | General Electric Company | Oil supply system with vacuum pump for transmission of drive system |
| US11629638B2 (en) | 2020-12-09 | 2023-04-18 | Supercritical Storage Company, Inc. | Three reservoir electric thermal energy storage system |
| US12331664B2 (en) | 2023-02-07 | 2025-06-17 | Supercritical Storage Company, Inc. | Waste heat integration into pumped thermal energy storage |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3527054A (en) * | 1969-01-23 | 1970-09-08 | Gen Electric | Pressurization of lubrication sumps in gas turbine engines |
| US3626693A (en) * | 1968-11-28 | 1971-12-14 | Jack Guillot | Device to ensure lubrication regulation and reliability of operation of gas turbines |
| US3779345A (en) * | 1972-05-22 | 1973-12-18 | Gen Electric | Emergency lubrication supply system |
| US4002224A (en) * | 1975-02-26 | 1977-01-11 | Westinghouse Electric Corporation | Turbine lubrication and emergency gas system |
| US4105093A (en) * | 1977-02-03 | 1978-08-08 | Westinghouse Electric Corp. | Control system for pressurized lubricating system |
| US4153141A (en) * | 1977-06-20 | 1979-05-08 | General Electric Company | Auxiliary oil supply system |
| US4157744A (en) * | 1977-07-18 | 1979-06-12 | Capriotti Lawrence J | Lubricating and cooling engine system component |
| US4171611A (en) * | 1975-08-07 | 1979-10-23 | Motoren- Und Turbinen-Union Munchen Gmbh | Vehicular gas turbine system |
| US4309870A (en) * | 1979-10-01 | 1982-01-12 | Carrier Corporation | Lubricating system for a turbomachine including a method of operating same |
-
1980
- 1980-12-18 US US06/217,572 patent/US4390082A/en not_active Expired - Lifetime
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3626693A (en) * | 1968-11-28 | 1971-12-14 | Jack Guillot | Device to ensure lubrication regulation and reliability of operation of gas turbines |
| US3527054A (en) * | 1969-01-23 | 1970-09-08 | Gen Electric | Pressurization of lubrication sumps in gas turbine engines |
| US3779345A (en) * | 1972-05-22 | 1973-12-18 | Gen Electric | Emergency lubrication supply system |
| US4002224A (en) * | 1975-02-26 | 1977-01-11 | Westinghouse Electric Corporation | Turbine lubrication and emergency gas system |
| US4171611A (en) * | 1975-08-07 | 1979-10-23 | Motoren- Und Turbinen-Union Munchen Gmbh | Vehicular gas turbine system |
| US4105093A (en) * | 1977-02-03 | 1978-08-08 | Westinghouse Electric Corp. | Control system for pressurized lubricating system |
| US4153141A (en) * | 1977-06-20 | 1979-05-08 | General Electric Company | Auxiliary oil supply system |
| US4157744A (en) * | 1977-07-18 | 1979-06-12 | Capriotti Lawrence J | Lubricating and cooling engine system component |
| US4309870A (en) * | 1979-10-01 | 1982-01-12 | Carrier Corporation | Lubricating system for a turbomachine including a method of operating same |
Cited By (46)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4511016A (en) * | 1982-11-16 | 1985-04-16 | Mtu Motoren-Und Turbinen-Union Muenchen Gmbh | Lubricating system for gas turbine engines |
| US4697414A (en) * | 1985-12-09 | 1987-10-06 | The Garrett Corporation | Lubrication apparatus |
| US4741155A (en) * | 1985-12-09 | 1988-05-03 | Allied-Signal Inc. | Lubrication method and apparatus |
| US4739862A (en) * | 1986-03-21 | 1988-04-26 | Mullis H Leon | Pressure lubricator |
| WO1988009874A1 (en) * | 1987-06-12 | 1988-12-15 | Kletschka Harold D | Rotary pump with a coupling section |
| US4844707A (en) * | 1987-06-12 | 1989-07-04 | Kletschka Harold D | Rotary pump |
| US4856273A (en) * | 1988-07-21 | 1989-08-15 | General Motors Corporation | Secondary oil system for gas turbine engine |
| US4858426A (en) * | 1988-07-21 | 1989-08-22 | General Motors Corporation | Secondary oil system for gas turbine engine |
| US4858427A (en) * | 1988-08-08 | 1989-08-22 | General Motors Corporation | Secondary oil system for gas turbine engine |
| US4891934A (en) * | 1988-10-31 | 1990-01-09 | General Motors Corporation | Oil system for gas turbine engine |
| US4888947A (en) * | 1988-10-31 | 1989-12-26 | General Motors Corporation | Secondary oil system |
| US5040366A (en) * | 1989-01-13 | 1991-08-20 | General Electric Company | Fluid transfer device |
| US5147015A (en) * | 1991-01-28 | 1992-09-15 | Westinghouse Electric Corp. | Seal oil temperature control method and apparatus |
| US5186277A (en) * | 1991-01-28 | 1993-02-16 | Westinghouse Electric Corp. | Generator sealing oil temperature control method and apparatus utilizing temperature matching |
| WO1999020880A1 (en) * | 1997-10-23 | 1999-04-29 | Carl Fredriksson | Device, method and application in connection with a turbomachine and pumping and lubricating arrangement in connection with such a machine |
| US6327857B1 (en) | 1997-10-23 | 2001-12-11 | Carl Fredriksson | Device, method and application in connection with a turbomachine and pumping and lubricating arrangement in connection with such a machine |
| US7216473B1 (en) * | 1999-07-09 | 2007-05-15 | Hamilton Sundstrand Corporation | Turbojet engine lubrication system |
| US7954599B2 (en) * | 2002-03-01 | 2011-06-07 | Flender Graffenstaden | Gear mechanism with controlled device for generating a rarefied atmosphere |
| US20050139427A1 (en) * | 2002-03-01 | 2005-06-30 | Alain Antonetti | Gear mechanism with controlledl device for generating a rarefied atmosphere |
| US20050000753A1 (en) * | 2003-07-03 | 2005-01-06 | Sheridan William G. | Failure tolerant passive lubrication system |
| US7174997B2 (en) | 2003-07-03 | 2007-02-13 | United Technologies Corporation | Failure tolerant passive lubrication system |
| US7387189B2 (en) | 2003-08-14 | 2008-06-17 | United Technologies Corp. | Emergency lubrication system |
| US20050034924A1 (en) * | 2003-08-14 | 2005-02-17 | James Denman H. | Emergency lubrication system |
| US20090057060A1 (en) * | 2007-08-28 | 2009-03-05 | Hamilton Sundstrand Corporation | Recirculating lubrication system with sealed lubrication oil storage |
| US8356694B2 (en) * | 2007-08-28 | 2013-01-22 | Pratt & Whitney | Recirculating lubrication system with sealed lubrication oil storage |
| US20090324151A1 (en) * | 2008-06-30 | 2009-12-31 | Nucor Corporation | Slew bearing system |
| US8002472B2 (en) | 2008-06-30 | 2011-08-23 | Nucor Corporation | Slew bearing system |
| US20110163018A1 (en) * | 2010-01-04 | 2011-07-07 | General Electric Company | Hydrogen cooled generator lubricant drain system |
| US8051953B2 (en) * | 2010-01-04 | 2011-11-08 | General Electric Company | Hydrogen cooled generator lubricant drain system |
| US9151327B2 (en) | 2010-06-11 | 2015-10-06 | Siemens Aktiengesellschaft | Backup lubrication system for a rotor bearing |
| US20130086903A1 (en) * | 2011-10-06 | 2013-04-11 | Gm Global Technology Operations Llc. | Engine assembly including fluid control to boost mechanism |
| US9127567B2 (en) | 2012-06-29 | 2015-09-08 | United Technologies Corporation | Non-interrupted turbomachine fluid supply |
| US10934895B2 (en) | 2013-03-04 | 2021-03-02 | Echogen Power Systems, Llc | Heat engine systems with high net power supercritical carbon dioxide circuits |
| EP3036470A4 (en) * | 2013-08-20 | 2016-08-17 | United Technologies Corp | Emergency oil system |
| US10570777B2 (en) * | 2014-11-03 | 2020-02-25 | Echogen Power Systems, Llc | Active thrust management of a turbopump within a supercritical working fluid circuit in a heat engine system |
| US20170314419A1 (en) * | 2014-11-03 | 2017-11-02 | Echogen Power Systems, L.L.C. | Active thrust management of a turbopump within a supercritical working fluid circuit in a heat engine system |
| US11293309B2 (en) | 2014-11-03 | 2022-04-05 | Echogen Power Systems, Llc | Active thrust management of a turbopump within a supercritical working fluid circuit in a heat engine system |
| US11187112B2 (en) | 2018-06-27 | 2021-11-30 | Echogen Power Systems Llc | Systems and methods for generating electricity via a pumped thermal energy storage system |
| US11293313B2 (en) * | 2018-09-19 | 2022-04-05 | Saudi Arabian Oil Company | Turbomachinery lubrication system improvement gravity rundown tanks |
| US20220205374A1 (en) * | 2018-09-19 | 2022-06-30 | Saudi Arabian Oil Company | Turbomachinery lubrication system improvement gravity rundown tanks |
| US11834972B2 (en) * | 2018-09-19 | 2023-12-05 | Saudi Arabian Oil Company | Turbomachinery lubrication system improvement gravity rundown tanks |
| US11435120B2 (en) | 2020-05-05 | 2022-09-06 | Echogen Power Systems (Delaware), Inc. | Split expansion heat pump cycle |
| US11629638B2 (en) | 2020-12-09 | 2023-04-18 | Supercritical Storage Company, Inc. | Three reservoir electric thermal energy storage system |
| US20230030818A1 (en) * | 2021-07-30 | 2023-02-02 | General Electric Company | Oil supply system with vacuum pump for transmission of drive system |
| US11959542B2 (en) * | 2021-07-30 | 2024-04-16 | Ge Infrastructure Technology Llc | Oil supply system with vacuum pump for transmission of drive system |
| US12331664B2 (en) | 2023-02-07 | 2025-06-17 | Supercritical Storage Company, Inc. | Waste heat integration into pumped thermal energy storage |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4390082A (en) | Reserve lubricant supply system | |
| US4105093A (en) | Control system for pressurized lubricating system | |
| US5641280A (en) | Rotary screw compressor with shaft seal | |
| US4722663A (en) | Seal-off mechanism for rotating turbine shaft | |
| US4309870A (en) | Lubricating system for a turbomachine including a method of operating same | |
| CN104081070B (en) | Method of controlling a wind turbine and wind turbine | |
| US4569196A (en) | Lubrication system | |
| CA1172974A (en) | Method and apparatus for lubricating turbine bearings | |
| US3147821A (en) | Emergency bearing oil supply for a decelerating shaft | |
| US4424665A (en) | Lubricating system for a turbomachine including a method of operating same | |
| GB2211898A (en) | A lubricating system for a turbo-engine | |
| US4741675A (en) | Flow control system for a hydraulic pump | |
| US4606652A (en) | Shaft seal for turbomachinery | |
| US4058320A (en) | Generator seal oil supply system | |
| US5045711A (en) | Turboexpander-generator | |
| EP0277924B1 (en) | Improvement to the lubrication circuit of rotary vacuum pumps | |
| US5885004A (en) | Hydrostatically supported foil bearing | |
| US2421056A (en) | Conveyor control system | |
| US4071254A (en) | Static sealing mechanism for a compressor | |
| US3288166A (en) | Accumulator system | |
| US2973135A (en) | Seal for refrigerant compressor | |
| US4277221A (en) | Wicket gate bearing seal | |
| EP3853446B1 (en) | Turbomachinery lubrication system with gravity rundown tank and corresponding lubrication method | |
| RU2684358C1 (en) | Device for stabilization of pressure drop in gas pumping unit sealing system | |
| US2523310A (en) | Hydraulic thrust bearing |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: ROTOFLOW CORPORATION 2235 CARMELINA AVE., LOS ANGE Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:SWEARINGEN, JUDSON S.;REEL/FRAME:004100/0334 Effective date: 19830224 |
|
| STCF | Information on status: patent grant |
Free format text: PATENTED CASE |
|
| FEPP | Fee payment procedure |
Free format text: MAINTENANCE FEE REMINDER MAILED (ORIGINAL EVENT CODE: REM.); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY |
|
| FEPP | Fee payment procedure |
Free format text: SURCHARGE FOR LATE PAYMENT, PL 96-517 (ORIGINAL EVENT CODE: M176); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY |
|
| MAFP | Maintenance fee payment |
Free format text: PAYMENT OF MAINTENANCE FEE, 4TH YEAR, PL 96-517 (ORIGINAL EVENT CODE: M170); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY Year of fee payment: 4 |
|
| FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY |
|
| MAFP | Maintenance fee payment |
Free format text: PAYMENT OF MAINTENANCE FEE, 8TH YEAR, PL 96-517 (ORIGINAL EVENT CODE: M171); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY Year of fee payment: 8 |
|
| FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY Free format text: PAYER NUMBER DE-ASSIGNED (ORIGINAL EVENT CODE: RMPN); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY |
|
| MAFP | Maintenance fee payment |
Free format text: PAYMENT OF MAINTENANCE FEE, 12TH YR, SMALL ENTITY (ORIGINAL EVENT CODE: M285); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY Year of fee payment: 12 |
|
| AS | Assignment |
Owner name: ATLAS COPCO ROTOFLOW INC., WISCONSIN Free format text: CHANGE OF NAME;ASSIGNOR:ROTOFLOW CORPORATION (A TEXAS CORP);REEL/FRAME:015098/0241 Effective date: 19960319 Owner name: GE OIL & GAS OPERATIONS LLC, WISCONSIN Free format text: MERGER;ASSIGNORS:AC COMPRESSOR ACQUISITION LLC (OF DELAWARE);GE ROTOFLOW INC. (A TEXAS CORP);REEL/FRAME:015098/0245 Effective date: 20030331 Owner name: GE ROTOFLOW, INC., WISCONSIN Free format text: CHANGE OF NAME;ASSIGNOR:ROTOFLOW INC. ( A TEXAS CORP);REEL/FRAME:015098/0259 Effective date: 20000901 Owner name: ROTOFLOW INC., WISCONSIN Free format text: CHANGE OF NAME;ASSIGNOR:ATLAS COPCO ROTOFLOW INC. (A TEXAS CORP);REEL/FRAME:015098/0238 Effective date: 20000503 |